EP1153260B1 - Flugkörper zur bekämpfung von fahrzeugen mit aktivem selbstschutz - Google Patents
Flugkörper zur bekämpfung von fahrzeugen mit aktivem selbstschutz Download PDFInfo
- Publication number
- EP1153260B1 EP1153260B1 EP00904904A EP00904904A EP1153260B1 EP 1153260 B1 EP1153260 B1 EP 1153260B1 EP 00904904 A EP00904904 A EP 00904904A EP 00904904 A EP00904904 A EP 00904904A EP 1153260 B1 EP1153260 B1 EP 1153260B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- missile
- protection
- self
- active self
- vehicles
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/56—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information for dispensing discrete solid bodies
- F42B12/58—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles
- F42B12/62—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile
- F42B12/625—Cluster or cargo ammunition, i.e. projectiles containing one or more submissiles the submissiles being ejected parallel to the longitudinal axis of the projectile a single submissile arranged in a carrier missile for being launched or accelerated coaxially; Coaxial tandem arrangement of missiles which are active in the target one after the other
Definitions
- the invention relates to a missile according to the preamble of claim 1.
- the basic principle of the active self-protection systems is a sensor arrangement on the armored vehicles, which detects the approaching missile and a plate or splitter firing defensive munitions, which is triggered by the sensor assembly and the approaching missile damaged, destroyed or deflected from the trajectory.
- An effective antidote is to shoot two missiles in quick succession at the same target.
- the first missile would thereby trigger the active self-protection system, while the second missile would hit the unprotected target.
- a device is of a single soldier, the weapon z. B. shoot from the shoulder, not applicable.
- the missile for fighting vehicles with active self-protection according to the preamble of claim 1 is provided with a detachable attached to the missile tip, self-propelled device that separates at a suitable distance from the target of the missile and at such a distance from the front flies that the active self-protection system is triggered by the device without jeopardizing the subsequent missile.
- the device according to the invention is wholly or partially pushed over the usually located at the top of antitank missiles tubular extension, so that the length of the missile increases only slightly.
- the device according to the invention may further comprise means for increasing the Radarnizstrahlqueriteses, z. B. with a reflector or transponder, be provided to increase the visibility by the sensor arrangement of the active self-protection system.
- the distance of the missile to the target, in which the device according to the invention separates from the missile by means of self-propulsion, is determined, for example, by a distance sensor on the device or on the missile. It may be z. B. be a laser range finder, a radar distance meter or an optoelectronic distance sensor.
- the missile is fired from a launching device, which itself has a laser rangefinder, so the distance information is entered at start into the missile so that it starts the device according to the invention after a corresponding flight time. In contrast to their own distance sensors, the missile then only needs a timer.
- Figure 1 shows in four phases - 1A to 1D - the use of the missile according to the invention.
- the target in the form of a tank 1 is equipped with a missile-detecting sensor arrangement 2 and fragment-forming defense ammunition 3, 3 ', 3 "
- the missile 4 consists of a rocket motor 5 with tail 6 and a warhead 7.
- a Self-propelled device 9 is arranged at the front end 8 of the warhead 7 at the front end 8 of the warhead 7 at the front end 8 of the warhead 7 at the front end 8 of the warhead 7 at the front end 8 of the warhead 7 .
- the device 9 driven by a rocket motor 10, is moved away from the missile 4 in the direction of the tank 1.
- the missile 4 is now a tubular extension 11 can be seen on the previously the device 9 was attached.
- the device 9 has led to the sensor assembly 2 on the tank 1, the defense ammunition 3 'has triggered, which detonates at the location 12.
- the distance 13 between the device 9 and the missile 4 is so great that the missile 4 is not or only slightly endangered by the splinters of the detonating defense ammunition 3 '.
- FIG. 1D shows how the warhead 7 of the missile 4 impinges on the tank 1 without being previously destroyed by the defensive munition 3 '(see FIG. 1C).
- Fig. 2 shows the device 9 of Fig. 1 in section.
- a rocket propellant 17 which can be ignited by a lighter 18.
- a timer 19 is arranged, which is connected to the lighter 18 by a cable 20.
- the timer 19 is set before the start of the missile 4 via the terminal 21 by a corresponding electronics on the firing rack.
- the terminal 21 may be, for example, a self-releasing connector or an inductive receiver.
- Fig. 3 shows in the form of a sequence program, the function of the missile according to the invention. The times given are typical values for a very specific antitank missile.
- the indicated reference numbers refer to the parts of the missile 4 and the device 9 shown in FIGS. 1 and 2.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19905268A DE19905268A1 (de) | 1999-02-09 | 1999-02-09 | Flugkörper zur Bekämpfung von Fahrzeugen mit aktivem Selbstschutz |
DE19905268 | 1999-02-09 | ||
PCT/EP2000/000189 WO2000047945A1 (de) | 1999-02-09 | 2000-01-13 | Flugkörper zur bekämpfung von fahrzeugen mit aktivem selbstschutz |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1153260A1 EP1153260A1 (de) | 2001-11-14 |
EP1153260B1 true EP1153260B1 (de) | 2005-09-21 |
Family
ID=7896894
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00904904A Expired - Lifetime EP1153260B1 (de) | 1999-02-09 | 2000-01-13 | Flugkörper zur bekämpfung von fahrzeugen mit aktivem selbstschutz |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP1153260B1 (es) |
AT (1) | ATE305127T1 (es) |
DE (2) | DE19905268A1 (es) |
ES (1) | ES2246223T3 (es) |
WO (1) | WO2000047945A1 (es) |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1605365A (es) * | 1900-01-01 | |||
US2804823A (en) * | 1955-05-13 | 1957-09-03 | Jablansky Louis | Multiple unit projectile |
FR2280877A1 (fr) * | 1974-07-31 | 1976-02-27 | Renard Jean | Projectile lanceur d'obus |
DE2948542A1 (de) * | 1979-12-03 | 1984-04-12 | Rheinmetall GmbH, 4000 Düsseldorf | Geschoss zum bekaempfen mehrlagiger, vorzugsweise aktiver panzerungen |
DE3004047C2 (de) * | 1980-02-05 | 1984-10-31 | Rheinmetall GmbH, 4000 Düsseldorf | Panzerbrechendes Geschoß |
DE3309147A1 (de) * | 1983-03-15 | 1984-09-20 | Rainer Dipl.-Phys. 6901 Gaiberg Berthold | Verfahren und anordnung zur korrektur eines zuendzeitpunktes |
SE449528B (sv) * | 1983-05-13 | 1987-05-04 | Bofors Ab | Pansarbrytande projektil |
US4567829A (en) * | 1984-07-30 | 1986-02-04 | General Electric Company | Shaped charge projectile system |
US4638737A (en) * | 1985-06-28 | 1987-01-27 | The United States Of America As Represented By The Secretary Of The Army | Multi-warhead, anti-armor missile |
DE3633535C1 (de) * | 1986-10-02 | 1996-09-26 | Daimler Benz Aerospace Ag | Gefechtskopf |
DE4022820A1 (de) * | 1990-07-18 | 1992-01-23 | Rheinmetall Gmbh | Unterkalibriges wuchtgeschoss |
DE4117871C1 (de) * | 1991-05-31 | 1999-08-19 | Diehl Stiftung & Co | Gefechtkopf gegen eine reaktive Zielpanzerung |
DE4217185C1 (de) * | 1992-05-23 | 1993-10-21 | Deutsche Aerospace | Flugkörper |
DE4331236C1 (de) * | 1993-09-15 | 1996-09-19 | Daimler Benz Aerospace Ag | Gefechtskopf zur Bekämpfung gepanzerter Ziele |
DE19505629B4 (de) | 1995-02-18 | 2004-04-29 | Diehl Stiftung & Co.Kg | Schutzeinrichtung gegen ein anfliegendes Projektil |
-
1999
- 1999-02-09 DE DE19905268A patent/DE19905268A1/de not_active Withdrawn
-
2000
- 2000-01-13 EP EP00904904A patent/EP1153260B1/de not_active Expired - Lifetime
- 2000-01-13 AT AT00904904T patent/ATE305127T1/de not_active IP Right Cessation
- 2000-01-13 WO PCT/EP2000/000189 patent/WO2000047945A1/de active IP Right Grant
- 2000-01-13 DE DE50011213T patent/DE50011213D1/de not_active Expired - Lifetime
- 2000-01-13 ES ES00904904T patent/ES2246223T3/es not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE50011213D1 (de) | 2006-02-02 |
ES2246223T3 (es) | 2006-02-16 |
EP1153260A1 (de) | 2001-11-14 |
DE19905268A1 (de) | 2000-08-10 |
WO2000047945A1 (de) | 2000-08-17 |
ATE305127T1 (de) | 2005-10-15 |
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